Explore the Engineering Database more efficiently by signing up for free. Sign up free

Thigh-Tangent-Angle-Rotorcraft-Min — Seating Geometry

Name: Mil1333B Cockpit Geometry — seating_geometry: dimension id thigh_tangent_angle_rotorcraft_min · description Thigh tangent angle minimum for rotorcraft · value in 5 inches or degrees (see unit column) · para ref Figure 2 Note 1 · figure ref Figure 2
Creator: Engineering Database

Category: Seating Geometry
Dimension Id: Thigh Tangent Angle Rotorcraft Min
Aircraft Applicability: Rotorcraft
Description: Thigh Tangent Angle Minimum for Rotorcraft
Figure Ref: Figure 2
Para Ref: Figure 2 Note 1
Qualifier: Min
Standard: MIL-Std-1333B
Unit: Degrees
Value in (inches or degrees (see unit column)): 5

Source: MIL-STD-1333B

Browse more aerospace engineering reference tables →